DocumentCode
841673
Title
On the feasibility of real-time prediction of aircraft carrier motion at sea
Author
Sidar, Menahem M. ; Doolin, Brian F.
Author_Institution
NASA, Moffett Field, CA, USA
Volume
28
Issue
3
fYear
1983
fDate
3/1/1983 12:00:00 AM
Firstpage
350
Lastpage
356
Abstract
Landing aircraft on board carriers is a most delicate phase of flight operations at sea. The ability to predict the aircraft carrier´s motion over an interval of several seconds within reasonable error bounds may allow an improvement in touchdown dispersion and reduce the value of the ramp clearance due to a smoother aircraft trajectory. Also, improved information to the landing signal officer should decrease the number of waveoffs substantially. This paper indicates and shows quantitatively that, based upon the power density spectrum data for pitch and heave measured for various ships and sea conditions, the motion can be predicted well for up to 15 s. Moreover, the zero crossover times for both pitch and heave motions can be predicted with impressive accuracy. The predictor was designed on the basis of Kalman´s optimum filtering theory (the discrete time case), being compatible with real-time digital computer operation.
Keywords
Aircraft landing guidance; Kalman filtering, linear systems; Marine-vehicle control; Motion measurements; Prediction methods; Accuracy; Aircraft; Density measurement; Filtering theory; Kalman filters; Marine vehicles; Motion measurement; Power measurement; Sea measurements; Trajectory;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.1983.1103227
Filename
1103227
Link To Document